WO2020012778A1 - Vanne d'injection de carburant - Google Patents

Vanne d'injection de carburant Download PDF

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Publication number
WO2020012778A1
WO2020012778A1 PCT/JP2019/019426 JP2019019426W WO2020012778A1 WO 2020012778 A1 WO2020012778 A1 WO 2020012778A1 JP 2019019426 W JP2019019426 W JP 2019019426W WO 2020012778 A1 WO2020012778 A1 WO 2020012778A1
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WO
WIPO (PCT)
Prior art keywords
injection hole
axis
injection
section
fuel
Prior art date
Application number
PCT/JP2019/019426
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English (en)
Japanese (ja)
Inventor
雅之 丹羽
陽介 中川
正寛 大隈
典嗣 加藤
浩毅 金田
Original Assignee
株式会社デンソー
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 株式会社デンソー filed Critical 株式会社デンソー
Priority to CN201980045949.4A priority Critical patent/CN112368475B/zh
Priority to DE112019003552.5T priority patent/DE112019003552T5/de
Publication of WO2020012778A1 publication Critical patent/WO2020012778A1/fr
Priority to US17/142,631 priority patent/US11835020B2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10—Other injectors with elongated valve bodies, i.e. of needle-valve type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/1833—Discharge orifices having changing cross sections, e.g. being divergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/184—Discharge orifices having non circular sections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/104—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on a side position of the cylinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00—Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • F02M51/0685—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature and the valve being allowed to move relatively to each other or not being attached to each other

Definitions

  • the present disclosure relates to a fuel injection valve that injects fuel.
  • the injection hole for injecting fuel has a flat shape. Specifically, when a virtual line extending along the center of the injection hole is called an injection hole axis, and a cross section of the injection hole that is perpendicular to the injection hole axis is called an injection hole vertical section, Are formed in a flat shape.
  • the fuel flowing through the injection hole does not flow while filling the entire vertical cross section of the injection hole, but flows while partially filling a region along the inner wall surface of the injection hole in the vertical cross section of the injection hole. That is, the fuel flowing from the inlet of the injection hole flows through the injection hole in a state of a liquid film along the inner wall surface of the injection hole, and is injected from the outlet of the injection hole.
  • the vertical cross section of the injection hole has a tapered shape whose area gradually increases from the inlet to the outlet of the injection hole. This also achieves atomization and low penetration of the spray.
  • the shape of the vertical cross section of the injection hole changes in a complicated manner depending on the cross section at any position on the injection hole axis. Therefore, when forming the injection hole by performing laser processing, drilling, or the like on the nozzle body, it is difficult to form the shape of the injection hole vertical cross section according to the position on the injection hole axis into a desired shape. It is difficult to form the injection hole into a desired shape. Then, the deterioration of the accuracy of the injection hole shape causes the deterioration of the accuracy of the spray shape.
  • the shape of the vertical cross section (inlet cross section) of the injection hole at the inlet of the injection hole has a great effect on how fuel flows into the injection hole. And shape. Therefore, the deterioration of the shape accuracy of the cross section of the inlet greatly affects the deterioration of the accuracy of the spray shape.
  • the shape of the vertical cross section of the injection hole changes in a complicated manner according to the position of the cross section on the injection hole axis.
  • the shape of the inlet cross section is likely to vary, and the accuracy of the spray shape is likely to deteriorate.
  • the present disclosure has an object to provide a fuel injection valve capable of realizing a shape in which an injection hole gradually increases in area and a flat shape while suppressing deterioration in accuracy of a spray shape.
  • a fuel injection valve includes: An injection hole capable of injecting fuel, a nozzle body having a fuel passage communicating with the injection hole, and a needle for switching between fuel injection from the injection hole and injection stop by opening and closing the fuel passage,
  • An injection hole axis a virtual line extending along the center of the injection hole
  • a cross section of the injection hole perpendicular to the injection hole axis is called an injection hole vertical cross section
  • the vertical cross section of the injection hole is a flat shape, and the shape gradually increases in area from the inlet to the outlet of the injection hole while maintaining a similar shape.
  • the vertical cross section of the injection hole has a flat shape and a shape whose area gradually increases from the inflow port to the outflow port of the injection hole while maintaining a similar shape. Therefore, the shape of the vertical cross section of the injection hole is similar regardless of the cross section at any position on the injection hole axis. Therefore, compared to the conventional shape in which the shape of the injection hole vertical cross section changes in a complicated manner according to the position on the injection hole axis, the shape of the injection hole vertical cross section corresponding to the position on the injection hole axis is a desired shape. Processing into a shape is facilitated. Therefore, it is possible to realize a shape in which the injection hole gradually increases in area and a flat shape while suppressing the deterioration in the spray shape accuracy due to the deterioration in the injection hole shape accuracy.
  • the variation in the shape of the injection hole vertical cross-section (inlet cross-section) at the inflow port of the injection hole due to the variation in the plate thickness of the nozzle body is suppressed by forming the similar shape as described above. Deterioration of the spray shape accuracy can be effectively suppressed.
  • a fuel injection valve includes a nozzle body having an injection hole capable of injecting fuel, and a fuel passage communicating with the injection hole, and opening and closing the fuel passage to form an injection valve.
  • a needle that switches between fuel injection from the hole and injection stop When a virtual line extending along the center of the injection hole is called an injection hole axis, and a cross section of the injection hole perpendicular to the injection hole axis is called an injection hole vertical cross section,
  • the vertical cross section of the injection hole is a shape that gradually expands in area from the inflow port to the outflow port while maintaining an elliptical shape having a short axis and a long axis.
  • the injection hole has a shape in which the ratio of the length of the short axis to the length of the long axis is constant from the inlet to the outlet.
  • the vertical cross section of the injection hole has a shape in which the area gradually increases while maintaining an elliptical shape from the inflow port to the outflow port, and the injection hole has a short axis length from the inflow port to the outflow port.
  • the ratio of the length to the length of the long axis is invariable. Therefore, compared to the conventional shape in which the shape of the injection hole vertical cross section changes in a complicated manner according to the position on the injection hole axis, the shape of the injection hole vertical cross section corresponding to the position on the injection hole axis is a desired shape. Processing into a shape is facilitated. Therefore, it is possible to realize a shape in which the injection hole gradually increases in area and an elliptical shape while suppressing the deterioration in accuracy of the spray shape due to the deterioration in accuracy of the injection hole shape.
  • FIG. 2 is a diagram showing an engine mounting position of the fuel injection valve in FIG. 1.
  • FIG. 3 is a view taken in the direction of the arrow III in FIG. 2.
  • FIG. 4 is a sectional view taken along the line IV-IV in FIG. 1.
  • FIG. 5 is a sectional view taken along line VV in FIG. 4.
  • FIG. 6 is a sectional view taken along the line VI-VI in FIG. 5.
  • FIG. 3 is a perspective view illustrating the definition of the injection hole axis.
  • FIG. 3 is a perspective view illustrating the definition of the injection hole axis.
  • FIG. 3 is a perspective view illustrating the definition of the injection hole axis.
  • FIG. 4 is a cross-sectional view schematically showing a difference in thickness of the nozzle body in the first embodiment.
  • FIG. 15 is a perspective view showing a difference in the shape of the inflow port corresponding to the difference in the thickness shown in FIG. 14.
  • FIG. 4 is a cross-sectional view schematically showing a difference in thickness of a nozzle body in a comparative example of the first embodiment.
  • FIG. 17 is a perspective view showing a difference in the shape of the inflow port corresponding to the difference in the thickness shown in FIG. 16.
  • FIG. 3 is a three-side view schematically illustrating the injection hole according to the first embodiment, and is a diagram illustrating a positional relationship between a focus of laser light and the injection hole.
  • the perspective view of FIG. FIG. 17 is a three-side view schematically showing the injection hole according to the comparative example shown in FIG.
  • FIG. 16 shows a positional relationship between the focus of the laser beam and the injection hole.
  • the perspective view of FIG. It is sectional drawing which shows the shape of the injection hole which concerns on 2nd Embodiment. It is a figure showing an engine mounting position of a fuel injection valve concerning a 3rd embodiment.
  • FIG. 24 is a view on arrow XXIV of FIG. 23. It is a perspective view explaining the shape of the injection hole concerning a 4th embodiment.
  • FIG. 26 is a cross-sectional view of FIG. 25 taken along the line XXVI-XXVI.
  • FIG. 27 is a cross-sectional view of FIG. 26 taken along the line XXVII-XXVII.
  • FIG. 29 is an enlarged view of FIG. 28. It is a figure showing distribution of fuel in the inflow mouth part of an injection hole in a comparative example of a 4th embodiment. It is a figure showing distribution of fuel in an inflow part of an injection hole in a 4th embodiment.
  • the fuel injection valve 1 shown in FIG. 1 is attached to an ignition ignition type vehicle internal combustion engine (engine E) shown in FIG.
  • the engine E includes a cylinder E1, a cylinder head E2, and a piston E3.
  • An intake valve E4, an exhaust valve E5, a spark plug E6, and a fuel injection valve 1 are attached to the cylinder head E2.
  • Two intake valves E4 and two exhaust valves E5 are attached.
  • the spark plug E6 is arranged on the central axis C1 of the piston E3.
  • the fuel injection valve 1 is disposed on the side of the intake valve E4 with respect to the center axis C1 and on the side of the piston E3 with respect to the intake valve E4, and is a side valve that directly injects fuel from the side of the combustion chamber Ea into the combustion chamber Ea. It is a jet type. Therefore, the center line C2 of the fuel injection valve 1 intersects the center axis C1 of the piston E3 at an angle of 45 degrees or more.
  • the arrows indicating the up-down direction in FIG. 2 do not indicate the up-down direction when the engine E is mounted on the vehicle, but indicate the compression side in the direction of the center axis C1 of the piston E3 as upper and the expansion side as lower. It is.
  • the fuel injection valve 1 has a plurality of injection holes 31 for injecting fuel.
  • the inflow port 311 of the injection hole 31 is arranged concentrically around the center line C2 of the fuel injection valve 1.
  • a virtual center line of the injection hole 31 extending from the center of the inflow port 311 of the injection hole 31 toward the center of the outflow port 312 of the injection hole 31 is referred to as an injection hole axis C3 described later in detail.
  • the direction of the fuel (spray) injected from the outlet 312 is the direction from the intake valve E4 side to the piston E3 side.
  • All the injection hole axes C3 are directed from the intake valve E4 side to the piston E3 side when viewed from the horizontal direction shown in FIG.
  • the fuel injection valve 1 includes the nozzle body 20, the needle 40, the movable core 47, the fixed core 44, the coil 38, the springs 24 and 26, and the like.
  • the movable core 47, the fixed core 44, and the coil 38 function as a driving unit that drives the needle 40 to open and close.
  • the high-pressure fuel supplied from the delivery pipe E7 (see FIG. 2) to the fuel injection valve 1 flows through the fuel passage 18 formed inside the nozzle body 20, and is injected from the injection hole 31.
  • the nozzle body 20 includes a first tubular member 21, a second tubular member 22, a third tubular member 23, and an injection nozzle 30.
  • the first tubular member 21, the second tubular member 22, and the third tubular member 23 are all substantially cylindrical members, and are coaxial in the order of the first tubular member 21, the second tubular member 22, and the third tubular member 23. And are connected to each other.
  • the injection nozzle 30 is provided at the end of the first cylinder member 21 opposite to the second cylinder member 22.
  • the injection nozzle 30 is a cylindrical member having a bottom and is welded to the first cylindrical member 21.
  • the injection nozzle 30 is subjected to a quenching treatment so as to have a predetermined hardness.
  • the injection nozzle 30 includes an injection unit 301 and a cylindrical unit 302.
  • the needle 40 is accommodated in the nozzle body 20 so as to be able to reciprocate in the direction of the center line C ⁇ b> 2, and the cylindrical portion 302 forms a cylindrical annular passage 305 with the outer surface of the needle 40.
  • the annular passage 305 extends annularly around the center line C2 and allows fuel to flow in the direction in which the center line C2 extends.
  • the injection unit 301 is a hollow hemispherical portion centered on a point on the center line C2 of the injection nozzle 30.
  • the injection unit 301 forms a hemispherical distribution passage 303 (suck chamber) between the injection unit 301 and the outer surface of the tip of the needle 40.
  • the upstream end of the distribution passage 303 communicates with the downstream end of the annular passage 305, and the downstream end of the distribution passage 303 communicates with the inflow port 311 of the injection hole 31.
  • the distribution passage 303 collects the fuel distributed in the annular shape through the annular passage 305 and distributes the collected fuel to the plurality of inflow ports 311.
  • the arrow in FIG. 4 indicates the flow direction of the fuel flowing from the annular passage 305 to the distribution passage 303, and flows from the outside in the radial direction toward the center line C2. A part of the fuel flowing in this way directly flows into the inflow port 311 of the injection hole 31, and another part flows into the inflow port 311 after being stored in the distribution passage 303.
  • the annular passage 305 and the distribution passage 303 constitute a part of the fuel passage 18 described above.
  • An annular valve seat 304 with which the needle 40 can abut is formed on the inner wall surface of the cylindrical portion 302.
  • the annular passage 305 is closed (closed), and the fuel injection from the injection hole 31 is stopped.
  • the annular passage 305 is released (opened), and fuel is injected from the injection hole 31.
  • the movable core 47 is a substantially cylindrical member that has been subjected to a magnetic stabilization process, and is engaged with the needle 40.
  • the fixed core 44 is a substantially cylindrical member that has been subjected to a magnetic stabilization process.
  • the fixed core 44 is welded to the third cylindrical member 23 of the nozzle body 20 and is fixed inside the nozzle body 20.
  • the coil 38 is a substantially cylindrical member, and is provided so as to mainly surround the radially outer sides of the second cylindrical member 22 and the third cylindrical member 23.
  • the coil 38 generates a magnetic field when electric power is supplied, and forms a magnetic circuit passing through the fixed core 44, the movable core 47, the first cylindrical member 21, and the third cylindrical member 23.
  • a magnetic attraction force is generated between the fixed core 44 and the movable core 47, the movable core 47 is attracted to the fixed core 44, and the needle 40 operates to open the valve.
  • the spring 24 urges the needle 40 together with the movable core 47 in the direction of the valve seat 304, that is, in the valve closing direction.
  • the spring 26 urges the movable core 47 in a direction opposite to the valve seat 304, that is, in a valve opening direction.
  • the urging force of the spring 24 is set to be larger than the urging force of the spring 26.
  • injection hole vertical cross sections S1, S2, S3, and S4 As shown in FIG. 5, a plane along the inflow port 311 and the outflow port 312 is not perpendicular to the injection hole axis C3 but is inclined.
  • the illustrated injection hole vertical cross section S1 is a cross section (inflow section) at the most upstream position of the injection hole 31 and is different from the opening shape of the inflow port 311.
  • the illustrated injection hole vertical cross section S4 is a cross section (outlet cross section) at the most downstream position of the injection hole 31 and is different from the opening shape of the outlet 312.
  • the vertical cross section of the injection hole is a flat shape at any position in the direction of the injection hole axis C3, and has a shape that gradually increases in area from the inflow port 311 to the outflow port 312 while maintaining a similar shape (see FIG. 7).
  • the vertical cross section of the injection hole has an elliptical shape having a short axis La and a long axis Lb from the inflow port 311 to the outflow port 312.
  • the ratio of the length of the short axis La to the length of the long axis Lb is the same at any position in the direction of the injection hole axis C3. That is, the injection hole 31 has a shape in which the ratio between the length of the short axis La and the length of the long axis Lb is invariable from the inflow port 311 to the outflow port 312.
  • a cross section of the injection hole 31 including the injection hole axis C3 is referred to as an injection hole longitudinal section, and a plane including the short axis La in the injection hole longitudinal section is referred to as a short axis plane (see FIG. 5).
  • a plane including the major axis Lb in the vertical section of the injection hole is called a major axis plane (see FIG. 6).
  • the vertical cross section of the injection hole has a tapered shape that linearly enlarges the inner wall surface of the injection hole 31 from the inflow port 311 to the outflow port 312.
  • the taper angle of the taper shape appearing on the short axis plane is called a short axis taper angle ⁇ a (see FIG. 5), and the taper angle of the taper shape appearing on the long axis plane is called a long axis taper angle ⁇ b (see FIG. 6).
  • a plurality of injection holes 31 are formed in the nozzle body 20, and the shapes shown in FIGS. 5 to 7 correspond to all the injection holes 31. These injection holes 31 are formed by performing laser processing on the nozzle body 20.
  • the imaginary straight lines L1, L2, and L3 indicated by dotted lines in FIGS. 9 and 10 are straight lines passing through any points of the three outlines R1, R2, and R3.
  • the first intersection P1 in the figure is the intersection of three virtual straight lines L1, L2, L3.
  • a virtual circle R4 indicated by a dotted line in FIG. 11 is a circle having a constant distance from the first intersection P1 and located on the inner wall surface of the injection hole 31.
  • Each of the virtual straight lines L4 and L5 in FIG. 12 is a straight line that bisects the circumferential length of the virtual circle R4.
  • the second intersection P2 in the drawing is the intersection of the two virtual straight lines L4 and L5. Then, as shown in FIG. 13, a straight line passing through the first intersection P1 and the second intersection P2 is defined as "injection hole axis C3".
  • the vertical cross section of the injection hole is an elliptical shape, and the area gradually increases from the inflow port 311 to the outflow port 312 of the injection hole 31 while maintaining a similar shape.
  • the vertical cross section of the injection hole has a shape in which the area gradually increases while maintaining an elliptical shape from the inflow port 311 to the outflow port 312, and the injection hole 31 has a short axis La from the inflow port 311 to the outflow port 312.
  • the shape is such that the ratio between the length and the length of the major axis Lb is invariable.
  • the shape of the injection hole vertical cross section corresponding to the position on the injection hole axis C3 is Laser processing into a desired shape is facilitated. Therefore, it is possible to realize a shape in which the area of the injection hole 31 is gradually increased and an elliptical shape while suppressing the deterioration of the spray shape accuracy due to the deterioration of the injection hole shape.
  • the fuel flowing through the injection hole 31 does not flow while filling the entire vertical cross section of the injection hole, but flows while partially filling a region along the inner wall surface of the injection hole in the vertical cross section of the injection hole. That is, the fuel flowing from the inflow port 311 of the injection hole 31 flows through the injection hole 31 in a state of a liquid film along the inner wall surface of the injection hole and is injected from the outlet 312. Therefore, by making the injection hole 31 elliptical as in the present embodiment, the liquid film is made thinner. As a result, the fuel (spray) injected from the outlet 312 can be atomized and the penetration can be reduced.
  • the injection hole vertical cross section has a shape in which the area gradually increases from the inflow port 311 to the outflow port 312 of the injection hole 31. This also achieves atomization and low penetration of the spray.
  • the shape of the injection hole vertical section S ⁇ b> 1 is illustrated as being the same as the opening shape of the inflow port 311.
  • the dashed lines ⁇ , ⁇ , and ⁇ in FIG. 14 indicate a state in which the thickness of the injection portion 301 of the injection nozzle 30 is different due to manufacturing variations. In other words, the thinner the wall thickness, the shorter the length of the injection hole 31 in the direction of the injection hole axis C3, and the position of the injection hole vertical section S1 (inflow section) approaches the injection hole vertical section S2 (outflow section). .
  • the solid line S1 ( ⁇ ) shown in the upper part of FIG. 15 shows the cross section of the inflow port when the thickness of the injection unit 301 is the thickness shown by the one-dot chain line ⁇ .
  • FIG. 15 shows the cross section of the inflow port when the thickness of the injection unit 301 is the thickness shown by the one-dot chain line ⁇ .
  • the solid line S1 ( ⁇ ) shown in the lower part of FIG. 15 shows the cross section of the inflow port when the thickness of the injection unit 301 is the thickness shown by the one-dot chain line ⁇ .
  • the shape of the injection hole vertical cross section according to the present embodiment is similar regardless of the cross section at any position on the injection hole axis C3, and the ratio of the short axis La / the long axis Lb is unchanged. Therefore, even if the thickness of the injection part 301 varies as shown by the one-dot chain lines ⁇ , ⁇ , and ⁇ , the shape of the inflow port cross section differs only in size, and the short axis La / long axis Lb ratio is the same. (See FIG. 15).
  • the ratio between the short axis taper angle ⁇ a and the long axis taper angle ⁇ b is the same as the ratio between the length of the short axis La and the length of the long axis Lb.
  • the injection part 301x and the injection hole 31x of the injection nozzle 30x shown in FIG. 16 show a comparative example of the present embodiment, and the shape of the injection hole vertical cross-section depends on the position on the injection hole axis C3. It changes non-similarly.
  • the short axis / long axis ratio of the nozzle hole vertical cross section changes according to the position on the nozzle hole axis C3. Therefore, when the thickness of the injection part 301x varies as shown by the dashed lines ⁇ , ⁇ , and ⁇ , the shape of the inflow port cross section differs in size, and the short axis / major axis ratio also changes (see FIG. 17). .
  • FIGS. 18 and 19 show the laser beam processing at the focal points P11 and P12 of the laser beam when the laser beam is emitted from the outflow port 312 toward the inflow port 311 in laser processing the injection hole 31 according to the present embodiment. Show.
  • the shape of the vertical cross section of the injection hole according to the present embodiment is similar regardless of the cross section at any position on the injection hole axis C3, and the ratio of the short axis La / the long axis Lb is unchanged. Therefore, the two intersection distances L11 and L12 described below are the same.
  • intersection distance L11 is a distance from a point (focal point P11) extending and intersecting the inner wall surface of the injection hole 31 appearing in the short-axis cross section to the injection hole vertical cross section S2 (outlet cross section).
  • the intersection distance L12 is a distance from a point (focal point P12) that extends and intersects the inner wall surface of the injection hole 31 appearing in the long-axis cross section to the injection hole vertical cross section S2 (outlet cross section).
  • the focal point P11 of the laser beam for laser processing the inner wall surface of the injection hole 31 appearing on the short-axis section coincides with the focal point P12 of the laser beam for laser processing the inner wall surface of the injection hole 31 appearing on the long-axis cross section. Therefore, the injection hole 31 can be laser-processed by turning an injection nozzle (not shown) for emitting laser light on the same plane as shown by an arrow Y1 without moving in the direction of the injection hole axis C3.
  • the two intersection distances L11 and L12 are different. Therefore, the focal point P11 of the laser beam which laser-processes the inner wall surface of the injection hole 31 appearing in the short-axis cross section does not coincide with the focal point P12 of the laser beam which laser-processes the inner wall surface of the injection hole 31 which appears in the long-axis cross section.
  • the injection hole 31 can be laser-processed by turning the injection nozzle that emits the laser light in the direction of the injection hole axis C3 as shown by the arrow Y2 while turning it as shown by the arrow Y1.
  • the injection nozzle can be turned by rotating the injection nozzle without moving in the injection hole axis C3 direction. Therefore, compared to the comparative example that requires turning while moving in the direction of the injection hole axis C3, the shape of the injection hole vertical cross section that expands according to the position on the injection hole axis C3 is changed to a desired shape. Processing becomes easier.
  • the shape of the cross section of the inflow port of the injection hole 31 varies due to the variation in the plate thickness of the nozzle body 20, as described above. It is suppressed by forming a similar shape and making the short axis / major axis ratio unchanged. Therefore, it is possible to effectively suppress the deterioration of the accuracy of the spray shape.
  • the vertical cross section of the injection hole according to the present embodiment has a tapered shape that linearly enlarges the inner wall surface of the injection hole 31 from the inflow port 311 to the outflow port 312. Therefore, laser processing can be facilitated as compared with the case of a curved shape in which the inner wall surface is enlarged in a curved manner.
  • the inflow ports 311 of the plurality of injection holes 31 are arranged concentrically around the center line C2 of the nozzle body 20.
  • the fuel passage 18 extends annularly around the center line C2 and allows the fuel to flow in the direction in which the center line C2 extends.
  • the fuel passage 18 collects the fuel flowing through the annular passage 305 to form a plurality of inlets 311. And a distribution passage 303 for distribution. Therefore, it is possible to promote equalization of the flow rate of the fuel flowing into each of the injection holes 31, and it is possible to suppress the inflow rate unevenness.
  • the outlet 312 of the injection hole 31 is located on the outer surface of the injection unit 301.
  • the concave portion 32 is formed on the outer surface 301a of the injection portion 301, and the injection hole 31 is formed in the concave portion 32. Therefore, the outflow port 312 of the injection hole 31 is located at a position deeper on the inflow port 311 side than the outer surface 301 a of the injection unit 301.
  • the recess 32 has a cylindrical shape formed coaxially with the injection hole axis C3.
  • the shape of the vertical cross section of the injection hole is similar to that of the first embodiment regardless of the cross section at any position on the injection hole axis C3, and the ratio of the short axis La / the long axis Lb is obtained. Is immutable.
  • the imaginary line L20 in FIG. 22 is obtained by extending the surface of the valve seat 304, and a part of the imaginary line L20 is located inside the injection hole 31. Therefore, the fuel flowing into the distribution passage 303 from the annular passage 305 along the valve seat 304 (see the arrow Y10) collides with the inner wall surface 31a of the inner wall surface of the injection hole 31 which is closer to the center line C2, and flows into the inlet port. 311 (see arrow Y11). Therefore, thinning of the fuel (see arrow Y12) flowing through the injection hole 31 in a state of a liquid film along the inner wall surface 31a is promoted.
  • the fuel injection valve 1 according to the first embodiment is a side direct injection type that injects fuel directly from a side of the combustion chamber Ea into the combustion chamber Ea.
  • the fuel injection valve 1 according to the present embodiment is a center direct injection type in which fuel is directly injected from above the combustion chamber Ea into the combustion chamber Ea, as shown in FIG.
  • the fuel injection valve 1 is disposed between the intake valve E4 and the exhaust valve E5, and the center line C2 of the fuel injection valve 1 has an angle of less than 45 degrees with respect to the center axis C1 of the piston E3.
  • the inlets 311 of the plurality of injection holes 31 are arranged concentrically around the center line C2 of the fuel injection valve 1.
  • the direction of the fuel (spray) injected from the outlet 312 is a direction that spreads radially outward from the center line C2.
  • All the injection hole axes C3 are in a direction away from the center line C2 as the downstream side of the injection hole 31 is located.
  • the shape of the vertical cross section of the injection hole according to the present embodiment is similar to that of the first embodiment, regardless of the cross section at any position on the injection hole axis C3, and the short axis La / The ratio of the long axis Lb is unchanged.
  • the vertical cross section of the injection hole is elliptical.
  • the injection hole vertical cross section has different lengths of the long axes Lbin and Lbout while sharing the short axis La from the inflow port 311 to the outflow port 312. It is a shape combining two semi-ellipses. Of the two semi-ellipses, the semi-ellipses closer to the center line C2 of the nozzle body 20 are called inner semi-ellipses S1in and S2in, and the other semi-ellipses are called outer semi-ellipses S1out and S2out.
  • the injection hole 31 has a shape in which the major axis Lbout of the outer semi-ellipses S1out and S2out is longer than the major axis Lbin of the inner semi-ellipses S1in and S2in over the entirety of the inflow port 311 to the outflow port 312.
  • the shape of the injection hole 31 on the short axis plane is symmetrical about the injection hole axis C3.
  • the shape of the injection hole 31 in the long axis plane is asymmetrical about the injection hole axis C3.
  • the inner wall surface of the injection hole 31 closer to the center line C2 is referred to as an inner wall surface 31b, and the wall surface farther from the center line C2 is referred to as an outer wall surface 31c.
  • an angle formed between the inner wall surface 31b and the injection hole axis C3 is referred to as an inner taper angle ⁇ 1
  • an angle formed between the outer wall surface 31c and the injection hole axis C3 is referred to as an outer taper angle ⁇ 2.
  • the inner taper angle ⁇ 1 is set to a value smaller than the outer taper angle ⁇ 2.
  • the inner taper angle and the outer taper angle are the same.
  • a line passing through the center of gravity or the center of the inflow port 311 is referred to as a virtual line L10.
  • the angle at which the imaginary line L10 intersects the injection hole axis C3 and which is viewed from the direction of the center line C2 is referred to as a torsion angle ⁇ 3.
  • the direction of fuel flowing from the annular passage 305 to the distribution passage 303 and flowing toward the inflow port 311 is parallel to the imaginary line L10.
  • the direction of the fuel flowing toward the inflow port 311 does not coincide with the direction of the fuel injection from the outflow port 312, and is twisted.
  • the degree of twist is indicated by the twist angle ⁇ 3.
  • the torsion angle ⁇ 3 of the injection hole 31 (1) is about 90 degrees
  • the torsion angle ⁇ 3 of the injection hole 31 (2) is less than 90 degrees (an acute angle)
  • the injection hole 31 is 180 degrees (obtuse angle)
  • the twist angle ⁇ 3 of the injection hole 31 (4) is zero degree. It can be said that the closer the twist angle ⁇ 3 is to 90 degrees, the greater the degree of twist. That is, among the four types of injection holes 31 shown in FIG. 28, the degree of twist of the injection hole 31 (1) is the largest.
  • FIG. 30 is a top view of the injection hole 31y according to the comparative example having a shape contrary to the present embodiment as viewed from the inflow port 311y side.
  • the hatched lines in the figure indicate the fuel distributed in the injection holes 31y.
  • the flow rate flowing into the outer semi-ellipse S1out is larger than the flow rate flowing into the inner semi-ellipse S1in. Therefore, the fuel that spreads along the inner wall surface of the injection hole tends to be unevenly distributed to the portion of the outer semi-ellipse S1out, and the liquid film in the region F indicated by the one-dot chain line tends to be thick.
  • the shape of the vertical cross section of the injection hole is similar regardless of the cross section at any position on the injection hole axis C3, and the short axis La / The ratio of the long axis Lb is unchanged. Therefore, the same effect as in the first embodiment is exerted.
  • the vertical cross section of the injection hole is elliptical, but the vertical cross section of the injection hole may not be elliptical as long as it is flat.
  • the vertical cross section of the injection hole has a tapered shape in which the inner wall surface of the injection hole 31 is linearly enlarged from the inflow port 311 to the outflow port 312.
  • the vertical cross section of the injection hole may have a curved shape in which the inner wall surface is curvedly enlarged from the inflow port 311 to the outflow port 312.
  • laser processing when laser processing the injection hole 31, laser light is emitted from the outlet 312 toward the inlet 311.
  • laser processing may be performed by emitting laser light from the inlet 311 to the outlet 312.
  • the number of the injection holes 31 is six, but may be a plurality other than six, or may be one.
  • the outer semi-ellipse S1out and the long axis Lbout of the outer semi-ellipse S2out are assumed to be the inner semi-ellipse S1in on the assumption that the injection hole vertical cross section is similar and the short axis La / long axis Lb ratio is invariable. , S2in longer than the long axis Lbin.
  • the vertical cross section of the injection hole may have a non-similar shape or the minor axis La / length
  • the shape in which the axis Lb ratio changes may be used.
  • the inner taper angle ⁇ 1 is smaller than the outer taper angle ⁇ 2 on the assumption that the vertical cross section of the injection hole is similar and the ratio of the short axis La / the long axis Lb is invariable.
  • the injection hole vertical cross section may have a non-similar shape or a shape in which the ratio of the short axis La / the long axis Lb may be changed. .

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

L'invention concerne un corps de buse (20) qui comporte un trou d'injection (31) qui peut injecter du carburant, et un passage de carburant (18) qui mène au trou d'injection. Une aiguille (40) ouvre et ferme le passage de carburant pour commuter entre l'injection de carburant depuis le trou d'injection et l'arrêt de l'injection. Un axe de trou d'injection (C3) est une ligne imaginaire qui s'étend à travers le centre du trou d'injection. Des sections transversales (S1, S2, S3, S4) perpendiculaires au trou d'injection sont des sections transversales du trou d'injection prises perpendiculairement à l'axe de trou d'injection. Les sections transversales perpendiculaires au trou d'injection présentent une forme plate et sont façonnées de telle sorte que les zones des sections transversales augmentent progressivement de l'entrée (311) vers la sortie (312) du trou d'injection tandis que les sections transversales sont maintenues dans des formes similaires.
PCT/JP2019/019426 2018-07-12 2019-05-16 Vanne d'injection de carburant WO2020012778A1 (fr)

Priority Applications (3)

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CN201980045949.4A CN112368475B (zh) 2018-07-12 2019-05-16 燃料喷射阀
DE112019003552.5T DE112019003552T5 (de) 2018-07-12 2019-05-16 Kraftstoffeinspritzventil
US17/142,631 US11835020B2 (en) 2018-07-12 2021-01-06 Fuel injection valve

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2018-132562 2018-07-12
JP2018132562A JP2020008013A (ja) 2018-07-12 2018-07-12 燃料噴射弁

Related Child Applications (1)

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US17/142,631 Continuation US11835020B2 (en) 2018-07-12 2021-01-06 Fuel injection valve

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WO2020012778A1 true WO2020012778A1 (fr) 2020-01-16

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US (1) US11835020B2 (fr)
JP (1) JP2020008013A (fr)
CN (1) CN112368475B (fr)
DE (1) DE112019003552T5 (fr)
WO (1) WO2020012778A1 (fr)

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JP7419997B2 (ja) * 2020-07-14 2024-01-23 株式会社デンソー 燃料噴射弁

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US11835020B2 (en) 2023-12-05
JP2020008013A (ja) 2020-01-16
CN112368475A (zh) 2021-02-12
DE112019003552T5 (de) 2021-04-01
CN112368475B (zh) 2023-02-10
US20210123403A1 (en) 2021-04-29

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